T-6 Boldface Ops Limits

Front 1

Emergency engine shutdown on the ground

Back 1

PCL - OFF

FIREWALL SHUTOFF HANDLE - PULL

Front 2

Abort

Back 2

PCL - IDLE

BRAKES - AS REQUIRED

Front 3

Engine failure immediately after takeoff (sufficient runway remaining straight ahead)

Back 3

AIRSPEED - 110 KNOTS (MINIMUM)

PCL - AS REQUIRED

EMER LDG GR HANDLE - PULL (AS REQUIRED)

Front 4

Engine failure during flight

Back 4

ZOOM/GLIDE - 125 KNOTS (MINIMUM)

PCL - OFF

INTERCEPT ELP

Front 5

Immedate airstart

Back 5

PCL - OFF

STARTER SWITCH - AUTO/RESET

PCL - IDLE, ABOVE 13% N1

Front 6

Uncommanded power changes / loss of power / uncommanded propeller feather

Back 6

PCL - MID RANGE

PMU SWITCH - OFF

PROP SYS CIRCUIT BREAKER (left front console) - PULL, IF Np STABLE BELOW 40%

Front 7

Inadvertent departure from controlled flight

Back 7

PCL - IDLE

CONTROLLS - NEUTRAL

ALTITUDE - CHECK

Front 8

Fire in flight if fire is confirmed

Back 8

PCL - OFF

FIREWALL SHUTOFF HANDLE - PULL

Front 9

Obogs inoperative

Back 9

GREEN RING - PULL (AS REQUIRED)

Front 10

Eject

Back 10

EJECTION HANDLE - PULL

Front 11

Max torque takeoff / max_________%

Back 11

100

Front 12

Torque transient______% (______seconds)

Back 12

131, 20

Front 13

Torque above _____% is indicative of a system malfunction

Back 13

102

Front 14

ITT idle _____*c

Back 14

750

Front 15

Max itt takeoff / max _____*c

Back 15

820

Front 16

Transient itt ____*c (up to ____seconds)

Back 16

870, 20

Front 17

N1 idle _____% to _____ % ground

Back 17

60, 61

Front 18

N1 ___% (min) flight

Back 18

67

Front 19

Np idle ____ to ____ %

Back 19

46, 50

Front 20

Np takeoff / max ____% (___%+-____% pmu off)

Back 20

100, 100, 2

Front 21

Avoid stabilized ground operations from ____ to _____ % Np

Back 21

62, 80

Front 22

Oil pressure takeoff / max _____ to ____psi

Back 22

90, 120

Front 23

Oil pressure aerobatics / spins ____ to _____ psi

Back 23

40, 130

Front 24

Oil pressure aerobatics / spins (idle) ____ to _____psi ( ___sec)

Back 24

15, 40 , 5

Front 25

Oil temp takeoff / max ____ to ____*c

Back 25

10, 105

Front 26

Oil temp transient ____ to _____ *c (___ minnutes)

Back 26

106, 110, 10

Front 27

Prohibibted manuvers _____________ stalls / spins

Back 27

Inverted

Front 28

Aggravated ______________

Back 28

Spins past two turns

Front 29

Spins with the pcl___________

Back 29

Above idle

Front 30

Spins with the _____,______, or ______ extended

Back 30

Landing gear, flaps, speed brakes

Front 31

Spins with the _________

Back 31

Pmu off

Front 32

Spins below _______ feet pressure altitude

Back 32

10,000

Front 33

Spins above _______ feet pressure altitude

Back 33

22,000

Front 34

Abrupt_______ manuvers

Back 34

Cross-controlled (snap)

Front 35

Aerobatic manuvers, spins, or stalls with greater than ________ pounds fuel imballence

Back 35

50

Front 36

_______ slides

Back 36

Tail

Front 37

Max airspeed gear and or flaps _____kias

Back 37

150

Front 38

Max operating speed ______ kias or ____ mach

Back 38

316, 0.67

Front 39

Full rudder deflection above _____ kias will exceed the limits of the rudder control system

Back 39

150

Front 40

Starter limits:

____seconds

Wait _____ sec, _____ min, _____ min , ______ min after each start attempt

Back 40

20, 30sec, 2 min, 5 min, 30 min

Front 41

Max itt for starting _____*c for ____seconds (do not attempt restart)

Back 41

1,000, 5

Front 42

Max oil pressure for start _____ psi

Back 42

200

Front 43

Min oil tempreature for starting ______*c

Back 43

-40

Front 44

Min battery voltage for starting

Back 44

23.5

Front 45

Pressureization normal above 18,000 ft ms

_____+- _____psi

Back 45

3.6, 0.2

Front 46

Overpressureziation valve opens ____psi

Back 46

4.0

Front 47

Normal recovery fuel_______ pounds

Back 47

200

Front 48

Minimum fuel _____ (_____ pounds solo)

Back 48

150, 200

Front 49

Emergency fuel _________ pounds (______ pounds solo)

Back 49

100, 100

Front 50

Minimum fuel for aerobatics _____ pounds per side

Back 50

150

Front 51

Minimum landing distance (lda) ______ feet or heavy weight flaps ____ landing distance plus ____ feet, whichever is geater.

Back 51

4,000, up, 500

Front 52

Minimum runway width _____ feet

Back 52

75

Front 53

Max crosswind dry runway

Back 53

25 knots

Front 54

Max croswind wet runway

Back 54

10 knots

Front 55

Max cross wind icy runway

Back 55

5 knots

Front 56

Max crosswind touch and go

Back 56

20 knots

Front 57

Max crosswind formation takeoff / landing

Back 57

15 knots

Front 58

Max tailwind component for takeoff

Back 58

10 knots

Front 59

Max wind with canopy open

Back 59

40 knots

Front 60

Acceleration limit symetric clean _____ to _____g's

Back 60

-3.5, 7.0

Front 61

Acceleration limit symetric gear and flaps ____ to _____ g's

Back 61

0, 2.5

Front 62

Acceleration limit asymmetric clean ____ to ____ g's

Back 62

-1.0, 4.7

Front 63

Acceleration limits asymetric gear / flaps _____ to _____ g's

Back 63

0, 2.0

Front 64

Intentional spin min altitude entry_____ feet msl

Back 64

13,500

Front 65

Intentional spin min cloud clearence _____ feet above clouds

Back 65

7,000

Front 66

Maximum icing band / icing type ______ feet / _______

Back 66

5,000, light rime

Front 67

Ground operation is limited to ambient temperatures of _____ to ______ *c

Back 67

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